US20150109696A1 - Solar reflector plate - Google Patents

Solar reflector plate Download PDF

Info

Publication number
US20150109696A1
US20150109696A1 US14/391,420 US201314391420A US2015109696A1 US 20150109696 A1 US20150109696 A1 US 20150109696A1 US 201314391420 A US201314391420 A US 201314391420A US 2015109696 A1 US2015109696 A1 US 2015109696A1
Authority
US
United States
Prior art keywords
reflector plate
reflective layer
sheet
steel
solar reflector
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
US14/391,420
Other versions
US9594191B2 (en
Inventor
Kazumichi Sashi
Takahiko Oshige
Shin Ishikawa
Yoshihito Sakamoto
Takahiro Kubota
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JFE Steel Corp
Original Assignee
JFE Steel Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by JFE Steel Corp filed Critical JFE Steel Corp
Assigned to JFE STEEL CORPORATION reassignment JFE STEEL CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ISHIKAWA, SHIN, KUBOTA, TAKAHIRO, OSHIGE, TAKAHIKO, SAKAMOTO, YOSHIHITO, SASHI, KAZUMICHI
Publication of US20150109696A1 publication Critical patent/US20150109696A1/en
Application granted granted Critical
Publication of US9594191B2 publication Critical patent/US9594191B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • B32B15/09—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin comprising polyesters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/18—Layered products comprising a layer of metal comprising iron or steel
    • C—CHEMISTRY; METALLURGY
    • C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
    • C09D183/00—Coating compositions based on macromolecular compounds obtained by reactions forming in the main chain of the macromolecule a linkage containing silicon, with or without sulfur, nitrogen, oxygen, or carbon only; Coating compositions based on derivatives of such polymers
    • C09D183/04—Polysiloxanes
    • C09D183/08—Polysiloxanes containing silicon bound to organic groups containing atoms other than carbon, hydrogen, and oxygen
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B1/00—Optical elements characterised by the material of which they are made; Optical coatings for optical elements
    • G02B1/10—Optical coatings produced by application to, or surface treatment of, optical elements
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B1/00—Optical elements characterised by the material of which they are made; Optical coatings for optical elements
    • G02B1/10—Optical coatings produced by application to, or surface treatment of, optical elements
    • G02B1/14—Protective coatings, e.g. hard coatings
    • G—PHYSICS
    • G02—OPTICS
    • G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B5/00—Optical elements other than lenses
    • G02B5/08—Mirrors
    • G02B5/0808—Mirrors having a single reflecting layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00—Coating on the layer surface
    • B32B2255/06—Coating on the layer surface on metal layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00—Coating on the layer surface
    • B32B2255/10—Coating on the layer surface on synthetic resin layer or on natural or synthetic rubber layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00—Coating on the layer surface
    • B32B2255/20—Inorganic coating
    • B32B2255/205—Metallic coating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00—Coating on the layer surface
    • B32B2255/26—Polymeric coating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2255/00—Coating on the layer surface
    • B32B2255/28—Multiple coating on one surface
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/40—Properties of the layers or laminate having particular optical properties
    • B32B2307/416—Reflective
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/712—Weather resistant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2457/00—Electrical equipment
    • B32B2457/12—Photovoltaic modules
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G77/00—Macromolecular compounds obtained by reactions forming a linkage containing silicon with or without sulfur, nitrogen, oxygen or carbon in the main chain of the macromolecule
    • C08G77/04—Polysiloxanes
    • C08G77/14—Polysiloxanes containing silicon bound to oxygen-containing groups
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G77/00—Macromolecular compounds obtained by reactions forming a linkage containing silicon with or without sulfur, nitrogen, oxygen or carbon in the main chain of the macromolecule
    • C08G77/04—Polysiloxanes
    • C08G77/22—Polysiloxanes containing silicon bound to organic groups containing atoms other than carbon, hydrogen and oxygen
    • C08G77/26—Polysiloxanes containing silicon bound to organic groups containing atoms other than carbon, hydrogen and oxygen nitrogen-containing groups

Definitions

  • This disclosure relates to a solar reflector plate suitably used for solar power generation.
  • optical reflector those obtained by depositing a thin film of a metal such as aluminum or silver on the front or back surface of a glass substrate having excellent smoothness have been used.
  • JP 62-57904 B proposes a reflective heat collector plate obtained by providing a reflective metal (aluminum, silver, or the like) deposition film onto the surface of a metal plate (aluminum, stainless steel, or the like), and coating the outer surface of the metal deposition film with a protective film of a transparent inorganic substance (SiO, SiO 2 , or the like).
  • JP 57-4003 A proposes a reflector including a substrate formed of an appropriate material such as a metal or an alloy like aluminum, a steel plate, or stainless steel, or plastic, a metal reflective film deposited onto the substrate and formed of aluminum, silver, or the like, and a transparent inorganic protective film deposited onto the surface of the metal reflective film and formed of, for example, a vitreous film such as SiO or SiO 2 .
  • JP 57-125901 A proposes a reflector obtained by providing a laminate-like protective layer formed of elements including a coat formed of de-alkalized metal silicate and a resin coat directly stacked and deposited onto the above coat, onto a metal substrate having a reflective surface.
  • the reflector plates disclosed in JP '904 and JP '003 are excellent in weather resistance since they have a coat containing an inorganic material as a main component.
  • the reflector plates are used as a solar reflector plate frequently positioned in a region where dust flies such as a desert region, the resistance thereof against the flying sand is insufficient.
  • FIG. 1A to 1C are schematic cross-sectional views showing an example of our solar reflector plate.
  • Our solar reflector plate includes a substrate, a reflective layer provided onto the substrate, and a protective layer provided onto the reflective layer, wherein the protective layer contains silicon and an organic substance, contains silicon in an amount of 10% by mass to 60% by mass in terms of SiO 2 , and has 1.5 to 3.2 oxygen atoms on average that form a chemical bond with silicon.
  • a solar reflector plate 10 includes a substrate 1 , a reflective layer 2 provided onto the substrate 1 , and a protective layer 3 provided onto the reflective layer 2 .
  • the solar reflector plate 10 may include an interlayer 4 between the reflective layer 2 and the protective layer 3 .
  • a base layer 5 may be provided between the substrate 1 and the reflective layer 2 .
  • the shape of the solar reflector plate 10 shown in FIG. 1 has a planar shape
  • the shape of the solar reflector plate is not limited to the planar shape, and may have a curved shape such as a trough shape (gutter shape), and a parabolic shape.
  • the substrate that the solar reflector plate includes is not particularly limited and, for example, a substrate such as a steel sheet, a plastic sheet, a ceramic sheet, or a glass sheet can be used.
  • the steel sheet that can be suitably used is not particularly limited as long as it is a general steel sheet.
  • a stainless steel sheet is preferable since it is excellent in corrosion resistance of the back surface or sheared surface, and a cold-rolled steel sheet or a steel sheet plated with zinc or the like is preferable in view of economics and for the reason that corrosion resistance can be improved by coating or the like.
  • the surface of the substrate be smooth in view of reducing the surface roughness of the reflective layer and protective layer described later.
  • the substrate surface may be smoothened by rolling, skin pass, polishing such as sandpaper polishing, electrolytic polishing and electrolytic compound polishing, a method of coating the substrate surface with an organic substance and/or an inorganic substance, a method of laminating a smooth film by using an adhesive, a method of pasting a smooth film by thermal lamination, and the like.
  • polishing such as sandpaper polishing, electrolytic polishing and electrolytic compound polishing
  • a sheet thickness of the substrate is preferably 10 mm or less in view of facilitating a curved shaping, and more preferably 6 mm or less, particularly in view of the workability of the curved shaping.
  • the reflective layer that the solar reflector plate has is not particularly limited as long as it is a reflective layer containing a metal.
  • the metal examples include aluminum (Al), silver (Ag), and the like having a high reflectance, and in view of economics, Al is preferable.
  • the content of the metal in the reflective layer is preferably 50% by mass or more, more preferably 80% by mass or more, and even more preferably 90% by mass or more, in view of improving the reflectance.
  • the method of depositing the reflective layer onto the substrate is not particularly limited and, for example, methods such as deposition, sputtering, electroplating, hot-dip coating, and non-electrolytic plating can be applied.
  • the film thickness of the reflective layer is preferably 0.001 ⁇ m to 0.5 ⁇ m, and more preferably 0.01 ⁇ m to 0.2 ⁇ m, in view of reflectance improvement and uniformity.
  • the film thickness of the reflective layer is preferably about 5 ⁇ m to 200 ⁇ m, and in view of reflectance improvement, it is preferable to reduce the surface roughness of plating by rolling, skin pass, polishing, and the like.
  • the reflective layer it is possible to use a film or a glass sheet onto which a metal such as Al or Ag has been deposited or sputtered. In such a case, the reflective layer can be pasted to the substrate by an adhesive or thermal lamination.
  • the film include films containing a resin as a main component such as a PET film, a polyester film, a polyethylene film, a polypropylene film, a polyolefin film, a polyvinyl chloride film, a polyvinylidene chloride film, an acrylic resin film, a polyvinyl alcohol film, a polycarbonate film, a polystyrene film, a polyacrylonitrile film, an ethylene-vinyl acetate copolymer film, an ethylene-vinyl alcohol copolymer film, an ethylene-methacrylic acid copolymer film, a nylon film, an ionomer film, and a silicone film.
  • a resin as a main component such as a PET film, a polyester film, a polyethylene film, a polypropylene film, a polyolefin film, a polyvinyl chloride film, a polyvinylidene chloride film, an acrylic resin film, a polyvinyl alcohol
  • the surface roughness of the film is desirably low in view of the reflectance improvement.
  • the surface roughness is preferably 0.2 ⁇ m or less and more preferably 0.02 ⁇ m or less, in terms of an arithmetic mean roughness (Ra).
  • the thickness of the film is preferably 1 ⁇ m or more, and more preferably 5 ⁇ m or more, in view of inhibiting the influence of the surface roughness of the substrate and improving the reflectance.
  • the thickness of the film is preferably 5000 ⁇ m or less, and more preferably 500 ⁇ m or less, in view of economics.
  • the glass sheet is not particularly limited, but the surface roughness thereof is preferably 0.2 ⁇ m or less, and more preferably 0.02 ⁇ m or less, in terms of Ra.
  • the thickness of the glass sheet is not also particularly limited, the thickness is preferably 50 ⁇ m to 1000 ⁇ m, and more preferably 100 ⁇ m to 500 ⁇ m, in view of facilitating a curved shaping.
  • the protective layer that the solar reflector plate has is a specific protective layer containing silicon (Si) and an organic substance.
  • the protective layer is not easily scratched since it is formed of a hard material.
  • the protective layer is rather vulnerable to micro scratches caused by flying sand, and the transparency easily deteriorates.
  • the protective layer is easily scratched since the material is soft, and the sand resistance is inferior.
  • a protective layer which contains Si and an organic substance, and in which the content of Si (hereinafter, also called the “Si content”) is a specific value, and the number of oxygen (O) atoms binding to Si (hereinafter, also called the “Si-bound oxygen atom number”) is a specific value can maintain an excellent reflectance of the reflective layer and greatly improve sand resistance and weather resistance.
  • a content of Si in the protective layer is 10% by mass to 60% by mass, preferably 15% by mass to 50% by mass, and more preferably 20% by mass to 40% by mass in terms of SiO 2 .
  • Si content is within the above range, sand resistance and weather resistance become excellent. We believe that this is because the hardness resulting from Si is excellently balanced with the flexibility resulting from the organic substance.
  • the Si content in the protective layer can be quantitated by fluorescence X-ray analysis or ICP-AES analysis.
  • ICP-AES analysis a method of performing analysis by peeling or scraping off the protective layer can be used, and a portion accounting for about 50% or more of the thickness from the surface layer may be analyzed and used as a representative.
  • the protective layer is a thin film, sometimes the reflective layer or substrate may be mixed into the sample for analysis. However, if these (the mixed reflective layer or substrate) are quantitated by analysis and subtracted, the Si content of the protective layer can be quantitated.
  • Si and the organic substance may be dispersed (mixed) while forming a sea-island structure, and any of Si and the organic substance may form the portion corresponding to the island.
  • the portions corresponding to the islands be fine, since the sand resistance becomes better in this structure.
  • the diameter of the portions is preferably 100 nm or less, and more preferably 50 nm or less.
  • Si and the organic substance are preferably a complex or a hybrid forming a chemical bond at the molecular level, since the transparency increases.
  • the Si-bound oxygen atom number in the protective layer is 1.5 to 3.2, and preferably 1.7 to 2.7 on average.
  • Si-bound oxygen atom number is within the above range, sand resistance and weather resistance become excellent. It is considered that this is because crosslinking proceeds suitably, and an appropriate molecular structure is formed.
  • the average number of oxygen atoms forming a chemical bond with one Si atom refers to a value confirmed by solid-state NMR (Dipolar Decoupling method), and can be measured using, for example, JNM-ECA series manufactured by JEOL Ltd.
  • a protective layer for example, it is possible to use a silicone-based compound (silicone-based resin) in which a siloxane bond has been generated by crosslinking (curing) of a silane compound containing an alkoxysilyl group or a silanol group.
  • silane compound examples include monofunctional R 3 Si(OR) 1 , bifunctional R 2 Si(OR) 2 , trifunctional RiSi(OR) 3 , and tetrafunctional Si(OR) 4 (in each formula, R represents a hydrogen atom or an organic group). If the respective silane compounds differing in the number of functional group are used in an appropriate combination, the Si-bound oxygen atom number described above can be adjusted.
  • the raw material (silane compound) of the silicone-based resin as the protective layer include tetraalkoxysilanes such as tetramethoxysilane and tetraethoxysi-lane; trialkoxysilanes such as methyltrimethoxysilane, phenyltrimethoxysilane, methyltriethoxy-silane, phenyltriethoxysilane, n-propyltrimethoxysilane, n-propyltriethoxysilane, hexyltrimethox-ysilane, hexyltriethoxysilane, decyltrimethoxysilane, trifluoropropyltrimethoxysilane, vinyltri-methoxysilane, vinyltriethoxysilane, 2-(3,4-epoxycyclohexyl)ethyltrimethoxysilane, 3-glycidoxypropyltrimethoxy, vinyl
  • the organic substance in the protective layer is not particularly limited and may be derived from, for example, the functional group (for example, an alkyl group, a phenyl group, an epoxy group, a vinyl group, a methacryloyl group, or an acryloyl group) that the above-described silane compound has.
  • the organic substance may be an epoxy resin, an acrylic resin, a polyester resin, an olefin-based resin, and the like that are mixed or made into a complex with the silane compound not having been crosslinked or with the silicone-based resin having been crosslinked.
  • the organic substance may be optionally cured by heating or ultraviolet rays.
  • organic substance in the protective layer examples include an organic filler, a resin stabilizer, and the like, in view of improving handling ability such as slipperiness and improving coating hardness.
  • organic filler examples include polystyrene, polyacrylate, and the like. One kind of these may be used alone, or two or more kinds thereof may be used concurrently.
  • the resin stabilizer examples include a hindered amine-based light stabilizer; a benzotriazole-based ultraviolet absorber; an antioxidant based on phenol, phosphorus, or sulfur; and the like.
  • a hindered amine-based light stabilizer a benzotriazole-based ultraviolet absorber
  • an antioxidant based on phenol, phosphorus, or sulfur an antioxidant based on phenol, phosphorus, or sulfur; and the like.
  • One kind of these may be used alone, or two or more kinds thereof used concurrently.
  • the protective layer may contain other components in addition to Si and the organic substance.
  • the protective layer may contain an inorganic filler.
  • the inorganic filler examples include titanium oxide, calcium carbonate, zirconium oxide, alumina, magnesium oxide, zinc oxide, barium sulfate, calcium phosphate, and the like. One kind of these may be used alone, or two or more kinds thereof may be used concurrently.
  • the content of the components is not particularly limited as long as it is within a range that does not diminish the effect of our plates. However, the content is preferably about 15% or less in the protective layer.
  • An elastic modulus of the protective layer is preferably 0.10 GPa to 15 GPa, and more preferably 0.5 GPa to 10 GPa, since sand resistance becomes better.
  • the elastic modulus can be measured using, for example, a Picodenter HM500 manufactured by Fischer Instruments K.K.
  • a surface profile of the protective layer is preferably smooth, in view of light condensation rate.
  • a surface roughness of the protective layer is preferably 0.10 ⁇ m or less in terms of an arithmetic mean roughness (Ra), since reflecting components diffused are reduced, and a regular reflectance can be maintained at a higher value.
  • Ra can be measured based on JIS B0601 (2001).
  • the surface roughness of the protective layer can be adjusted to some extent by controlling surface profiles of the substrate or the reflective layer. Accordingly, to reduce the surface roughness of the protective layer, it is effective to reduce beforehand the surface roughness of the substrate or the reflective layer.
  • the surface roughness of the protective layer can also be adjusted by a method such as reducing a viscosity of a coating liquid for forming the protective layer, or increasing time allowed to elapse before curing is performed.
  • a method is also effective in which coating is performed by diluting the components with a solvent such as acetone, toluene, ethyl ether, methyl cellosolve, cellosolve, butyl cellosolve (ethylene glycol monobutyl ether), ethanol, isopropyl alcohol, propylene glycol 1-monomethyl ether 2-acetate, or water.
  • a solid content concentration at that time is preferably about 0.5% by mass to 50% by mass.
  • the thickness of the protective layer is not particularly limited. However, in view of balance between the reflectance and protection, the thickness is preferably 0.01 ⁇ m to 20 ⁇ m, more preferably 0.01 ⁇ m to 10 ⁇ m, and particularly preferably 0.1 ⁇ m to 5 ⁇ m.
  • the solar reflector plate include an interlayer between the reflective layer and the protective layer since the adhesiveness of the protective layer is improved, and the weather resistance becomes better in this manner.
  • the interlayer contains at least one kind selected from a group consisting of a silane coupling agent, a titanium coupling agent, a zirconium coupling agent, and an organic resin.
  • a film thickness of the interlayer is preferably about a thickness at a monolayer level (several angstroms) to 0.5 ⁇ m.
  • the thickness is preferably about 0.1 ⁇ m to 5 ⁇ m.
  • silane coupling agent examples include alkoxysilanes having a functional group such as a vinyl group, an epoxy group, a styryl group, a methacryloyl group, an acryloyl group, an amino group, a ureide group, a mercapto group, a sulfide group, or an isocyanate group.
  • a functional group such as a vinyl group, an epoxy group, a styryl group, a methacryloyl group, an acryloyl group, an amino group, a ureide group, a mercapto group, a sulfide group, or an isocyanate group.
  • titanium coupling agent examples include titanium tetraisopropoxide, titanium tetra-n-butoxide, titanium butoxide dimer, titanium tetra-2-ethylhexoxide, and the like.
  • zirconium coupling agent examples include zirconium acetate, zirconium ammonium carbonate, zirconium fluoride, and the like.
  • a silane coupling agent is preferable since it has excellent compatibility with the protective layer and makes it possible to improve the weather resistance and maintain the excellent reflectance of the reflective layer at a higher degree.
  • the interlayer When a silane coupling agent is used as the interlayer, the interlayer may be regarded as a portion of the protective layer, and an amount of the silane coupling agent that is expressed in terms of SiO 2 can be added to the Si content of the protective layer.
  • an organic resin for example, a vinyl chloride resin, a vinyl chloride acetate resin, an acrylic resin, a modified olefin resin, a polyester resin, a polycarbonate resin, and the like having excellent transparency and light resistance can be used.
  • At least one base layer constituted with an organic material and/or an inorganic material be provided between the substrate and the reflective layer, since the smoothness of the reflective layer is improved, and the reflectance is heightened in this manner.
  • the base layer constituted with an organic material include films containing a resin as a main component such as a PET film, a polyester film, a polyethylene film, a polypropylene film, a polyolefin film, a polyvinyl chloride film, a polyvinylidene chloride film, an acrylic resin film, a polyvinyl alcohol film, a polycarbonate film, a polystyrene film, a polyacrylonitrile film, an ethylene-vinyl acetate copolymer film, an ethylene-vinyl alcohol copolymer film, an ethylene-methacrylic acid copolymer film, a nylon film, an ionomer film, a silicone film, and the like.
  • a resin as a main component such as a PET film, a polyester film, a polyethylene film, a polypropylene film, a polyolefin film, a polyvinyl chloride film, a polyvinylidene chloride film, an acrylic
  • the base layer constituted with an inorganic material examples include a glass sheet, a glass coat, metal plating such as nickel or zinc, and the like.
  • the base layer, reflective layer, interlayer, and protective layer shown in Tables 1 to 3 were formed by the following method, thereby preparing solar reflector plates.
  • a cell marked with “-” indicates that the corresponding item is not provided (not treated).
  • the substrate shown in Tables 1 to 3 specifically the following substrates were used.
  • the substrate surface on which the reflective layer would be formed was subjected to skin pass finishing.
  • the base layer was pasted to the substrate by using an adhesive.
  • a film having an arithmetic mean roughness (Ra) of 0.1 ⁇ m and a thickness described in Tables 1 to 3 (50 ⁇ m if the thickness is not described in Tables 1 to 3) was used.
  • Example 50 As a glass sheet for the base layer used in Example 50, AN100 (sheet thickness 0.5 mm) manufactured by ASAHI GLASS CO., LTD. was used.
  • a glass coat for the base layer used in Example 54 a glass coat was used which was obtained by firing powdered glass for a low-temperature seal (BAS115, manufactured by ASAHI GLASS CO., LTD.) for 30 minutes at 500° C. to yield a thickness of 100 ⁇ m.
  • BAS115 manufactured by ASAHI GLASS CO., LTD.
  • the reflective layer was formed by depositing Al or Ag shown in Tables 1 to 3 onto the base layer. Further, regarding Example 60, the reflective layer was formed in a manner in which melted Al was plated onto the base layer such that the thickness thereof became 100 ⁇ m, and then mirror polishing was performed until the thickness thereof became 80 ⁇ m.
  • the thickness of the reflective layers not described in Tables 1 to 3 was 0.1 ⁇ m.
  • the interlayer was formed in a manner in which a 0.5% by mass aqueous solution in which the silane coupling agent or the like shown in Tables 1 to 3 was dissolved was coated onto the reflective layer at 10 g/m 2 , followed by drying for 5 minutes at 110° C.
  • the thickness of the respective interlayers was as described in Tables 1 to 3.
  • 3-glycidoxypropyltrimethoxysilane was used as a silane coupling agent
  • titanium tetraisopropoxide was used as a titanium coupling agent
  • zirconium ammonium carbonate was used as a zirconium coupling agent.
  • silane coupling agent marked with “#” 3-aminopropyltrimethoxysilane was used.
  • the protective layer was formed in a manner in which a coating liquid (solid content concentration 10% by mass), which was obtained by mixing the compounding agent shown in Table 4 and the curing agent shown in Table 5 with a solvent (ethylene glycol monobutyl ether) such that a mass ratio between them became the value shown in Tables 1 to 3, was coated onto the reflective layer (interlayer when the interlayer was provided) by using a bar coater, followed by heating and drying under the curing conditions shown in Tables 1 to 3.
  • a coating liquid solid content concentration 10% by mass
  • a solvent ethylene glycol monobutyl ether
  • the Si content (expressed in terms of SiO 2 ) was quantitated by alkali fusion/ICP-AES analysis by peeling the protective layer or scraping off the protective layer from the surface layer.
  • the Si-bound oxygen atom number was calculated from chemical shift of solid-state NMR (JNM-ECA series, manufactured by JEOL Ltd.). The results of these are shown in Tables 1 to 3 together with the measurement results of the elastic modulus, thickness, and arithmetic mean roughness (Ra).
  • a regular reflectance at a wavelength of 300 nm to 2500 nm was measured and evaluated as a solar radiation reflectance multiplied by a weighting coefficient based on JIS K5602 (2008).
  • a reflectance of 70% or higher was regarded as pass.
  • the solar reflector plates prepared in Examples 14 to 21, 24 to 31, 33 to 47, 49 to 50, and 61 to 71 in which a stainless steel sheet, a cold-rolled steel sheet, a hot-dip galvanized steel sheet, or an electrogalvanized steel sheet is used as a substrate, and the interlayer is provided between the reflective layer and protective layer, the sand resistance and weather resistance (particularly, weather resistance) tend to further improve.

Landscapes

  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Wood Science & Technology (AREA)
  • Organic Chemistry (AREA)
  • Optical Elements Other Than Lenses (AREA)
  • Laminated Bodies (AREA)
  • Paints Or Removers (AREA)

Abstract

A solar reflector plate maintains an excellent reflectance of a reflective layer and has excellent sand resistance and weather resistance. The solar reflector plate includes a substrate; a reflective layer provided onto the substrate; and a protective layer provided onto the reflective layer, wherein the protective layer contains silicon in an amount of 10% by mass to 60% by mass in terms of SiO2 and an organic substance, and has 1.5 to 3.2 oxygen atoms on average that form a chemical bond with silicon.

Description

    TECHNICAL FIELD
  • This disclosure relates to a solar reflector plate suitably used for solar power generation.
    • BACKGROUND
  • In the related art, as an optical reflector, those obtained by depositing a thin film of a metal such as aluminum or silver on the front or back surface of a glass substrate having excellent smoothness have been used.
  • When a thin metal film is deposited onto the surface of a glass substrate, a relatively high reflectance can be obtained. However, when this is used as a reflector plate for solar power generation (solar reflector plate), the plate is inevitably used outdoors. Accordingly, many problems regarding sand resistance, weather resistance, impact resistance, lightening of weight, and the like should be solved.
  • Regarding those problems, for example, JP 62-57904 B proposes a reflective heat collector plate obtained by providing a reflective metal (aluminum, silver, or the like) deposition film onto the surface of a metal plate (aluminum, stainless steel, or the like), and coating the outer surface of the metal deposition film with a protective film of a transparent inorganic substance (SiO, SiO2, or the like).
  • Moreover, JP 57-4003 A proposes a reflector including a substrate formed of an appropriate material such as a metal or an alloy like aluminum, a steel plate, or stainless steel, or plastic, a metal reflective film deposited onto the substrate and formed of aluminum, silver, or the like, and a transparent inorganic protective film deposited onto the surface of the metal reflective film and formed of, for example, a vitreous film such as SiO or SiO2.
  • In addition, JP 57-125901 A proposes a reflector obtained by providing a laminate-like protective layer formed of elements including a coat formed of de-alkalized metal silicate and a resin coat directly stacked and deposited onto the above coat, onto a metal substrate having a reflective surface.
  • We found that the reflector plates disclosed in JP '904 and JP '003 are excellent in weather resistance since they have a coat containing an inorganic material as a main component. However, if the reflector plates are used as a solar reflector plate frequently positioned in a region where dust flies such as a desert region, the resistance thereof against the flying sand is insufficient.
  • We also found that since the reflector plate disclosed in JP '901 includes a resin coat as an uppermost surface layer, the sand resistance thereof is very poor.
  • Accordingly, it could be helpful to provide a solar reflector plate which maintains an excellent reflectance of a reflective layer and has excellent sand resistance and weather resistance.
    • SUMMARY
  • We found that if a specific protective layer containing silicon and an organic substance is provided to a solar reflector plate, an excellent reflectance of a reflective layer is maintained, and sand resistance and weather resistance become excellent.
  • We thus provide the following (1) to (5):
      • (1) A solar reflector plate comprising:
        • a substrate;
        • a reflective layer provided onto the substrate; and
        • a protective layer provided onto the reflective layer,
        • wherein the protective layer contains silicon and an organic substance, contains silicon in an amount of 10% by mass to 60% by mass in terms of SiO2, and has 1.5 to 3.2 oxygen atoms on average that form a chemical bond with silicon.
      • (2) The solar reflector plate according to (1), wherein an elastic modulus of the protective layer is 0.1 GPa to 15 GPa.
      • (3) The solar reflector plate according to (1) or (2), wherein the reflective layer contains aluminum and/or silver.
      • (4) The solar reflector plate according to any one of (1) to (3), further comprising an interlayer containing at least one kind selected from a group consisting of a silane coupling agent, a titanium coupling agent, a zirconium coupling agent, and an organic resin, between the reflective layer and the protective layer.
      • (5) The solar reflector plate according to any one of (1) to (4), further comprising at least one base layer constituted with an organic material and/or an inorganic material, between the substrate and the reflective layer.
  • It is possible to provide a solar reflector plate which maintains an excellent reflectance of a reflective layer and has excellent sand resistance and weather resistance.
    • BRIEF DESCRIPTION OF THE DRAWING
  • FIG. 1A to 1C are schematic cross-sectional views showing an example of our solar reflector plate.
    •  DESCRIPTION OF SYMBOLS
    • 1: SUBSTRATE
    • 2: REFLECTIVE LAYER
    • 3: PROTECTIVE LAYER
    • 4: INTERLAYER
    • 5: BASE LAYER
    • 10: SOLAR REFLECTOR PLATE
    DETAILED DESCRIPTION
  • Our solar reflector plate includes a substrate, a reflective layer provided onto the substrate, and a protective layer provided onto the reflective layer, wherein the protective layer contains silicon and an organic substance, contains silicon in an amount of 10% by mass to 60% by mass in terms of SiO2, and has 1.5 to 3.2 oxygen atoms on average that form a chemical bond with silicon.
  • Next, the overall constitution of the solar reflector plate will be described using drawings.
  • As shown in FIGS. 1A to 1C, a solar reflector plate 10 includes a substrate 1, a reflective layer 2 provided onto the substrate 1, and a protective layer 3 provided onto the reflective layer 2.
  • Moreover, as shown in FIG. 1B, the solar reflector plate 10 may include an interlayer 4 between the reflective layer 2 and the protective layer 3.
  • In addition, as shown in FIG. 1C, a base layer 5 may be provided between the substrate 1 and the reflective layer 2.
  • Though the solar reflector plate 10 shown in FIG. 1 has a planar shape, the shape of the solar reflector plate is not limited to the planar shape, and may have a curved shape such as a trough shape (gutter shape), and a parabolic shape.
  • Next, regarding the respective constitutions of the solar reflector plate, the materials, formation methods, and the like will be described.
    • Substrate
  • The substrate that the solar reflector plate includes is not particularly limited and, for example, a substrate such as a steel sheet, a plastic sheet, a ceramic sheet, or a glass sheet can be used.
  • Among these, the steel sheet that can be suitably used is not particularly limited as long as it is a general steel sheet. However, a stainless steel sheet is preferable since it is excellent in corrosion resistance of the back surface or sheared surface, and a cold-rolled steel sheet or a steel sheet plated with zinc or the like is preferable in view of economics and for the reason that corrosion resistance can be improved by coating or the like.
  • It is preferable that the surface of the substrate be smooth in view of reducing the surface roughness of the reflective layer and protective layer described later.
  • The substrate surface may be smoothened by rolling, skin pass, polishing such as sandpaper polishing, electrolytic polishing and electrolytic compound polishing, a method of coating the substrate surface with an organic substance and/or an inorganic substance, a method of laminating a smooth film by using an adhesive, a method of pasting a smooth film by thermal lamination, and the like.
  • In addition, a sheet thickness of the substrate is preferably 10 mm or less in view of facilitating a curved shaping, and more preferably 6 mm or less, particularly in view of the workability of the curved shaping.
    • Reflective Layer
  • The reflective layer that the solar reflector plate has is not particularly limited as long as it is a reflective layer containing a metal.
  • Specific examples of the metal include aluminum (Al), silver (Ag), and the like having a high reflectance, and in view of economics, Al is preferable.
  • The content of the metal in the reflective layer is preferably 50% by mass or more, more preferably 80% by mass or more, and even more preferably 90% by mass or more, in view of improving the reflectance.
  • The method of depositing the reflective layer onto the substrate (a base layer if the solar reflector plate has the base layer described later) is not particularly limited and, for example, methods such as deposition, sputtering, electroplating, hot-dip coating, and non-electrolytic plating can be applied.
  • When deposition or sputtering is applied, the film thickness of the reflective layer is preferably 0.001 μm to 0.5 μm, and more preferably 0.01 μm to 0.2 μm, in view of reflectance improvement and uniformity.
  • Furthermore, when electroplating or hot-dip coating is applied, the film thickness of the reflective layer is preferably about 5 μm to 200 μm, and in view of reflectance improvement, it is preferable to reduce the surface roughness of plating by rolling, skin pass, polishing, and the like.
  • In addition, as the reflective layer, it is possible to use a film or a glass sheet onto which a metal such as Al or Ag has been deposited or sputtered. In such a case, the reflective layer can be pasted to the substrate by an adhesive or thermal lamination.
  • Specific examples of the film include films containing a resin as a main component such as a PET film, a polyester film, a polyethylene film, a polypropylene film, a polyolefin film, a polyvinyl chloride film, a polyvinylidene chloride film, an acrylic resin film, a polyvinyl alcohol film, a polycarbonate film, a polystyrene film, a polyacrylonitrile film, an ethylene-vinyl acetate copolymer film, an ethylene-vinyl alcohol copolymer film, an ethylene-methacrylic acid copolymer film, a nylon film, an ionomer film, and a silicone film.
  • Though not particularly limited, the surface roughness of the film is desirably low in view of the reflectance improvement. Specifically, the surface roughness is preferably 0.2 μm or less and more preferably 0.02 μm or less, in terms of an arithmetic mean roughness (Ra).
  • Moreover, though not particularly limited, the thickness of the film is preferably 1 μm or more, and more preferably 5 μm or more, in view of inhibiting the influence of the surface roughness of the substrate and improving the reflectance. Similarly, the thickness of the film is preferably 5000 μm or less, and more preferably 500 μm or less, in view of economics.
  • Meanwhile, the glass sheet is not particularly limited, but the surface roughness thereof is preferably 0.2 μm or less, and more preferably 0.02 μm or less, in terms of Ra.
  • Though the thickness of the glass sheet is not also particularly limited, the thickness is preferably 50 μm to 1000 μm, and more preferably 100 μm to 500 μm, in view of facilitating a curved shaping.
    • Protective Layer
  • The protective layer that the solar reflector plate has is a specific protective layer containing silicon (Si) and an organic substance.
  • It was believed that if a vitreous coat containing an inorganic substance as a main component is used as the protective layer, the protective layer is not easily scratched since it is formed of a hard material. However, we found that since the material is brittle, the protective layer is rather vulnerable to micro scratches caused by flying sand, and the transparency easily deteriorates.
  • Moreover, if silicone rubber or a silicone resin is used as the protective layer, the protective layer is easily scratched since the material is soft, and the sand resistance is inferior.
  • We found, however, that a protective layer which contains Si and an organic substance, and in which the content of Si (hereinafter, also called the “Si content”) is a specific value, and the number of oxygen (O) atoms binding to Si (hereinafter, also called the “Si-bound oxygen atom number”) is a specific value can maintain an excellent reflectance of the reflective layer and greatly improve sand resistance and weather resistance.
    • Si Content
  • A content of Si in the protective layer is 10% by mass to 60% by mass, preferably 15% by mass to 50% by mass, and more preferably 20% by mass to 40% by mass in terms of SiO2.
  • If the Si content is within the above range, sand resistance and weather resistance become excellent. We believe that this is because the hardness resulting from Si is excellently balanced with the flexibility resulting from the organic substance.
  • The Si content in the protective layer can be quantitated by fluorescence X-ray analysis or ICP-AES analysis. In ICP-AES analysis, a method of performing analysis by peeling or scraping off the protective layer can be used, and a portion accounting for about 50% or more of the thickness from the surface layer may be analyzed and used as a representative. In addition, when the protective layer is a thin film, sometimes the reflective layer or substrate may be mixed into the sample for analysis. However, if these (the mixed reflective layer or substrate) are quantitated by analysis and subtracted, the Si content of the protective layer can be quantitated.
  • There is a possibility that Si and the organic substance may be dispersed (mixed) while forming a sea-island structure, and any of Si and the organic substance may form the portion corresponding to the island.
  • Moreover, in the dispersed state of Si and the organic substance, it is preferable that the portions corresponding to the islands be fine, since the sand resistance becomes better in this structure. Specifically, the diameter of the portions is preferably 100 nm or less, and more preferably 50 nm or less.
  • Furthermore, Si and the organic substance are preferably a complex or a hybrid forming a chemical bond at the molecular level, since the transparency increases.
    • Si-Bound Oxygen Atom Number
  • The Si-bound oxygen atom number in the protective layer is 1.5 to 3.2, and preferably 1.7 to 2.7 on average.
  • If the Si-bound oxygen atom number is within the above range, sand resistance and weather resistance become excellent. It is considered that this is because crosslinking proceeds suitably, and an appropriate molecular structure is formed.
  • The average number of oxygen atoms forming a chemical bond with one Si atom refers to a value confirmed by solid-state NMR (Dipolar Decoupling method), and can be measured using, for example, JNM-ECA series manufactured by JEOL Ltd.
  • As such a protective layer, for example, it is possible to use a silicone-based compound (silicone-based resin) in which a siloxane bond has been generated by crosslinking (curing) of a silane compound containing an alkoxysilyl group or a silanol group.
  • Examples of the silane compound include monofunctional R3Si(OR)1, bifunctional R2Si(OR)2, trifunctional RiSi(OR)3, and tetrafunctional Si(OR)4 (in each formula, R represents a hydrogen atom or an organic group). If the respective silane compounds differing in the number of functional group are used in an appropriate combination, the Si-bound oxygen atom number described above can be adjusted.
  • Specific examples of the raw material (silane compound) of the silicone-based resin as the protective layer include tetraalkoxysilanes such as tetramethoxysilane and tetraethoxysi-lane; trialkoxysilanes such as methyltrimethoxysilane, phenyltrimethoxysilane, methyltriethoxy-silane, phenyltriethoxysilane, n-propyltrimethoxysilane, n-propyltriethoxysilane, hexyltrimethox-ysilane, hexyltriethoxysilane, decyltrimethoxysilane, trifluoropropyltrimethoxysilane, vinyltri-methoxysilane, vinyltriethoxysilane, 2-(3,4-epoxycyclohexyl)ethyltrimethoxysilane, 3-glycidoxypropyltrimethoxysilane, 3-glycidoxypropyltriethoxysilane, p-styryltrimethoxysilane, 3-acrylox-ypropyltrimethoxysilane, N-2-(aminoethyl)-3-aminopropyltrimethoxysilane, 3-aminopropyltrimethoxysilane, 3-ureidopropyltriethoxysilane, 3-mercaptopropyltrimethoxysilane, bis(triethoxy-silylpropyl)tetrasulfide, and 3-isocyanatopropyltriethoxysilane; dialkoxysilanes such as dimeth-yldimethoxysilane, dimethyldiethoxysilane, 3-glycidoxypropylmethyldimethoxysilane, 3-glycid-oxypropylmethyldiethoxysilane, 3-methacryloxypropylmethyldimethoxysilane, N-2-(aminoethyl)-3-aminopropylmethyldimethoxysilane, and 3-mercaptopropylmethyldimethoxysilane; chloro-silanes such as methyltrichlorosilane, dimethyldichlorosilane, trimethylchlorosilane, phenyltri-chlorosilane, trimethylsilyl chloride, and triethylsilyl chloride; silazanes such as hexamethyldisi-lazane; and the like. One kind of these may be used alone, or two or more kinds thereof may be used concurrently.
  • The organic substance in the protective layer is not particularly limited and may be derived from, for example, the functional group (for example, an alkyl group, a phenyl group, an epoxy group, a vinyl group, a methacryloyl group, or an acryloyl group) that the above-described silane compound has. In view of adjusting the Si content, the organic substance may be an epoxy resin, an acrylic resin, a polyester resin, an olefin-based resin, and the like that are mixed or made into a complex with the silane compound not having been crosslinked or with the silicone-based resin having been crosslinked.
  • When such a resin is used as the organic substance, the organic substance may be optionally cured by heating or ultraviolet rays.
  • Other examples of the organic substance in the protective layer include an organic filler, a resin stabilizer, and the like, in view of improving handling ability such as slipperiness and improving coating hardness.
  • Specific examples of the organic filler include polystyrene, polyacrylate, and the like. One kind of these may be used alone, or two or more kinds thereof may be used concurrently.
  • Specific examples of the resin stabilizer include a hindered amine-based light stabilizer; a benzotriazole-based ultraviolet absorber; an antioxidant based on phenol, phosphorus, or sulfur; and the like. One kind of these may be used alone, or two or more kinds thereof used concurrently.
  • The protective layer may contain other components in addition to Si and the organic substance. For example, in view of improving handling ability such as slipperiness and improving coating hardness, the protective layer may contain an inorganic filler.
  • Specific examples of the inorganic filler include titanium oxide, calcium carbonate, zirconium oxide, alumina, magnesium oxide, zinc oxide, barium sulfate, calcium phosphate, and the like. One kind of these may be used alone, or two or more kinds thereof may be used concurrently.
  • When the protective layer contains other components in addition to Si and the organic substance, the content of the components is not particularly limited as long as it is within a range that does not diminish the effect of our plates. However, the content is preferably about 15% or less in the protective layer.
  • An elastic modulus of the protective layer is preferably 0.10 GPa to 15 GPa, and more preferably 0.5 GPa to 10 GPa, since sand resistance becomes better.
  • The elastic modulus can be measured using, for example, a Picodenter HM500 manufactured by Fischer Instruments K.K.
  • Moreover, though not particularly limited, A surface profile of the protective layer is preferably smooth, in view of light condensation rate.
  • A surface roughness of the protective layer is preferably 0.10 μm or less in terms of an arithmetic mean roughness (Ra), since reflecting components diffused are reduced, and a regular reflectance can be maintained at a higher value. Ra can be measured based on JIS B0601 (2001).
  • The surface roughness of the protective layer can be adjusted to some extent by controlling surface profiles of the substrate or the reflective layer. Accordingly, to reduce the surface roughness of the protective layer, it is effective to reduce beforehand the surface roughness of the substrate or the reflective layer.
  • Furthermore, the surface roughness of the protective layer can also be adjusted by a method such as reducing a viscosity of a coating liquid for forming the protective layer, or increasing time allowed to elapse before curing is performed.
  • In addition, a method is also effective in which coating is performed by diluting the components with a solvent such as acetone, toluene, ethyl ether, methyl cellosolve, cellosolve, butyl cellosolve (ethylene glycol monobutyl ether), ethanol, isopropyl alcohol, propylene glycol 1-monomethyl ether 2-acetate, or water. A solid content concentration at that time is preferably about 0.5% by mass to 50% by mass.
  • Moreover, the thickness of the protective layer is not particularly limited. However, in view of balance between the reflectance and protection, the thickness is preferably 0.01 μm to 20 μm, more preferably 0.01 μm to 10 μm, and particularly preferably 0.1 μm to 5 μm.
    • Interlayer
  • It is preferable that the solar reflector plate include an interlayer between the reflective layer and the protective layer since the adhesiveness of the protective layer is improved, and the weather resistance becomes better in this manner.
  • The interlayer contains at least one kind selected from a group consisting of a silane coupling agent, a titanium coupling agent, a zirconium coupling agent, and an organic resin.
  • In addition, when a silane coupling agent, a titanium coupling agent, or a zirconium coupling agent is used, a film thickness of the interlayer is preferably about a thickness at a monolayer level (several angstroms) to 0.5 μm. When an organic resin is used, the thickness is preferably about 0.1 μm to 5 μm.
  • Examples of the silane coupling agent include alkoxysilanes having a functional group such as a vinyl group, an epoxy group, a styryl group, a methacryloyl group, an acryloyl group, an amino group, a ureide group, a mercapto group, a sulfide group, or an isocyanate group.
  • Examples of the titanium coupling agent include titanium tetraisopropoxide, titanium tetra-n-butoxide, titanium butoxide dimer, titanium tetra-2-ethylhexoxide, and the like.
  • Examples of the zirconium coupling agent include zirconium acetate, zirconium ammonium carbonate, zirconium fluoride, and the like.
  • Among these, a silane coupling agent is preferable since it has excellent compatibility with the protective layer and makes it possible to improve the weather resistance and maintain the excellent reflectance of the reflective layer at a higher degree.
  • When a silane coupling agent is used as the interlayer, the interlayer may be regarded as a portion of the protective layer, and an amount of the silane coupling agent that is expressed in terms of SiO2 can be added to the Si content of the protective layer.
  • Meanwhile, as an organic resin, for example, a vinyl chloride resin, a vinyl chloride acetate resin, an acrylic resin, a modified olefin resin, a polyester resin, a polycarbonate resin, and the like having excellent transparency and light resistance can be used.
    • Base Layer
  • It is preferable that in the solar reflector plate, at least one base layer constituted with an organic material and/or an inorganic material be provided between the substrate and the reflective layer, since the smoothness of the reflective layer is improved, and the reflectance is heightened in this manner.
  • Specific examples of the base layer constituted with an organic material include films containing a resin as a main component such as a PET film, a polyester film, a polyethylene film, a polypropylene film, a polyolefin film, a polyvinyl chloride film, a polyvinylidene chloride film, an acrylic resin film, a polyvinyl alcohol film, a polycarbonate film, a polystyrene film, a polyacrylonitrile film, an ethylene-vinyl acetate copolymer film, an ethylene-vinyl alcohol copolymer film, an ethylene-methacrylic acid copolymer film, a nylon film, an ionomer film, a silicone film, and the like.
  • Specific examples of the base layer constituted with an inorganic material include a glass sheet, a glass coat, metal plating such as nickel or zinc, and the like.
    • EXAMPLES
  • Hereinafter, our plates will be described in detail based on examples, but this disclosure is not limited to such examples.
    • Examples 1 to 71 and Comparative Examples 1 to 16
  • On the substrate shown in Tables 1 to 3, the base layer, reflective layer, interlayer, and protective layer shown in Tables 1 to 3 were formed by the following method, thereby preparing solar reflector plates.
  • In Tables 1 to 3, a cell marked with “-” indicates that the corresponding item is not provided (not treated). Moreover, as the substrate shown in Tables 1 to 3, specifically the following substrates were used. When any of a stainless steel sheet, a cold-rolled steel sheet, a hot-dip galvanized steel sheet, and an electrogalvanized steel sheet was used as the substrate, the substrate surface on which the reflective layer would be formed was subjected to skin pass finishing.
    • Substrate
      • Stainless steel sheet: SUS430 (sheet thickness 0.1 mm)
      • Cold-rolled steel sheet: SPCC (sheet thickness 0.35 mm)
      • Plastic substrate: vinyl chloride (sheet thickness 5 mm)
      • Ceramic substrate: fiber-reinforced cement sheet [flexible board (sheet thickness 5 mm, manufactured by Mitsubishi Materials Corporation.)
      • Glass substrate: float sheet glass (sheet thickness 5 mm, manufactured by ASAHI GLASS CO., LTD.)
      • Hot-dip galvanized steel sheet (sheet thickness 0.30 mm, both side plating, amount of plating deposit on each side: 100 g/m2)
      • Electrogalvanized steel sheet (sheet thickness 0.45 mm, both side plating, amount of plating deposit on each side: 20 g/m2)
    Base Layer
  • The base layer was pasted to the substrate by using an adhesive.
  • As a PET film for the base layer, a film having an arithmetic mean roughness (Ra) of 0.1 μm and a thickness described in Tables 1 to 3 (50 μm if the thickness is not described in Tables 1 to 3) was used.
  • As a glass sheet for the base layer used in Example 50, AN100 (sheet thickness 0.5 mm) manufactured by ASAHI GLASS CO., LTD. was used.
  • As a glass coat for the base layer used in Example 54, a glass coat was used which was obtained by firing powdered glass for a low-temperature seal (BAS115, manufactured by ASAHI GLASS CO., LTD.) for 30 minutes at 500° C. to yield a thickness of 100 μm.
    • Reflective Layer
  • The reflective layer was formed by depositing Al or Ag shown in Tables 1 to 3 onto the base layer. Further, regarding Example 60, the reflective layer was formed in a manner in which melted Al was plated onto the base layer such that the thickness thereof became 100 μm, and then mirror polishing was performed until the thickness thereof became 80 μm.
  • The thickness of the reflective layers not described in Tables 1 to 3 was 0.1 μm.
    • Interlayer
  • The interlayer was formed in a manner in which a 0.5% by mass aqueous solution in which the silane coupling agent or the like shown in Tables 1 to 3 was dissolved was coated onto the reflective layer at 10 g/m2, followed by drying for 5 minutes at 110° C. The thickness of the respective interlayers was as described in Tables 1 to 3.
  • 3-glycidoxypropyltrimethoxysilane was used as a silane coupling agent, titanium tetraisopropoxide was used as a titanium coupling agent, and zirconium ammonium carbonate was used as a zirconium coupling agent.
  • Moreover, as the silane coupling agent marked with “#,”3-aminopropyltrimethoxysilane was used.
    • Protective Layer
  • The protective layer was formed in a manner in which a coating liquid (solid content concentration 10% by mass), which was obtained by mixing the compounding agent shown in Table 4 and the curing agent shown in Table 5 with a solvent (ethylene glycol monobutyl ether) such that a mass ratio between them became the value shown in Tables 1 to 3, was coated onto the reflective layer (interlayer when the interlayer was provided) by using a bar coater, followed by heating and drying under the curing conditions shown in Tables 1 to 3. Regarding Comparative Examples 10 to 14, the compounding agents shown in Table 4 and the curing agents shown in Table 5 were not used, and the silicone rubber (RTV rubber KE-1842, curing conditions: 120° C.×1 hr, thickness 1 μm, manufactured by Shin-Etsu Chemical Co., Ltd.), a silicone resin (KR-300, curing conditions: 250° C.×1 hr, thickness 1 μm, manufactured by Shin-Etsu Chemical Co., Ltd.), a SiO2 deposition film, borosilicate glass, and metal silicate (lithium silicate LSS45, manufactured by NISSAN CHEMICAL INDUSTRIES, LTD.) were respectively used as shown in Table 1 to form the protective layer.
  • Regarding the formed protective layer, the Si content (expressed in terms of SiO2) was quantitated by alkali fusion/ICP-AES analysis by peeling the protective layer or scraping off the protective layer from the surface layer. The Si-bound oxygen atom number was calculated from chemical shift of solid-state NMR (JNM-ECA series, manufactured by JEOL Ltd.). The results of these are shown in Tables 1 to 3 together with the measurement results of the elastic modulus, thickness, and arithmetic mean roughness (Ra).
  • The respective solar reflector plates prepared were evaluated in terms of the reflectance, sand resistance, and weather resistance by the evaluation methods shown below. These results are shown in Tables 1 to 3.
    • Reflectance
  • By using a spectrophotometer (UV-3100PC, manufactured by Shimadzu Corporation), a regular reflectance at a wavelength of 300 nm to 2500 nm was measured and evaluated as a solar radiation reflectance multiplied by a weighting coefficient based on JIS K5602 (2008). A reflectance of 70% or higher was regarded as pass.
    • Sand Resistance
  • Based on JIS H8503 (1989), a reduction rate of the regular reflectance at the time when 2 kg of silicon carbide was dropped on the test surface was evaluated.
    • Criteria for Judgment
      • 1: 5% or less (pass)
      • 2: higher than 5% to 10% or less (pass)
      • 3: higher than 10% to 30% or less (failure)
      • 4: higher than 30% (failure)
    Weather Resistance
  • Based on JIS D0205 (1987), a reduction rate of the regular reflectance at the time when a sunshine weather test was performed for 1000 hours was evaluated.
    • Criteria for Judgment
      • 1: 5% or less (pass)
      • 2: higher than 5% to 10% or less (pass)
      • 3: higher than 10% to 30% or less (failure)
      • 4: higher than 30% (failure)
  • TABLE 1
    Protective layer Characteristics
    Interlayer SiO2 SiOn Elastic Cur- Re-
    Reflec- Thick- Con- Num- mod- Thick- ing flec- Sand Weather
    Sub- Base tive ness A B C D E F G V W Other verted ber ulus ness Ra condi- tance resis- resis-
    strate layer layer Type μm Parts by mass % of n GPa μm μm tions (%) tance tance
    Compar- Stain- PET Al — — Sili- 100 960 48 5 2.0 1.2 1.0 0.01 100° C. × 86.2 4 4
    ative less cone- 1 hr
    Exam- steel based
    ple 1 sheet com-
    pound
    Compar- Stain- PET Al — — Sili- 100 590 29.5 8 2.0 1.6 1.0 0.01 100° C. × 85.9 3 3
    ative less cone- 1 hr
    Exam- steel based
    ple 2 sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 100 460 23 10 2.0 2.1 1.0 0.01 100° C. × 87.1 2 2
    ple 1 less cone- 1 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 100 300 15 14 2.0 2.3 1.0 0.01 100° C. × 88.6 1 2
    ple 2 less cone- 1 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 100 210 10.5 19 2.0 2.8 1.0 0.01 100° C. × 88.4 1 2
    ple 3 less cone- 1 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 100 130 6.5 29 2.0 2.9 1.0 0.01 100° C. × 89.9 1 2
    ple 4 less cone- 1 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 100 90 4.5 38 2.0 3.0 1.0 0.01 100° C. × 88.2 1 2
    ple 5 less cone- 1 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 100 63 3.15 49 2.0 3.2 1.0 0.01 100° C. × 88.0 1 2
    ple 6 less cone- 1 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 100 47 2.35 58 2.0 3.1 1.0 0.01 100° C. × 87.8 2 2
    ple 7 less cone- 1 hr
    steel based
    sheet com-
    pound
    Compar- Stain- PET Al — — Sili- 100 35 1.75 68 2.0 2.8 1.0 0.01 100° C. × 86.4 3 2
    ative less cone- 1 hr
    Exam- steel based
    ple 3 sheet com-
    pound
    Compar- Stain- PET Al — — Sili- 100 30 1.5 73 2.0 2.3 1.0 0.01 100° C. × 87.5 4 3
    ative less cone- 1 hr
    Exam- steel based
    ple 4 sheet com-
    pound
    Compar- Stain- PET Al — — Sili- 100 170 300 15 29 1.2 0.1 1.0 0.01 100° C. × 85.9 4 4
    ative less cone- 1 hr
    Exam- steel based
    ple 5 sheet com-
    pound
    Compar- Stain- PET Al — — Sili- 100 120 250 12.5 29 1.3 0.4 1.0 0.01 100° C. × 87.3 3 3
    ative less cone- 1 hr
    Exam- steel based
    ple 6 sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 100 50 180 9 29 1.5 0.7 1.0 0.01 100° C. × 89.1 2 2
    ple 8 less cone- 1 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 100 20 150 7.5 29 1.7 1.2 1.0 0.01 100° C. × 88.7 1 2
    ple 9 less cone- 1 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 50 100 185 9.25 29 2.3 2.5 1.0 0.01 100° C. × 87.9 1 2
    ple 10 less cone- 1 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 200 100 350 17.5 29 2.7 2.9 1.0 0.01 100° C. × 87.6 1 2
    ple 11 less cone- 1 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 600 100 795 39.75 29 2.9 4.4 1.0 0.01 100° C. × 87.4 2 2
    ple 12 less cone- 1 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 30 100 135 6.75 29 3.2 5.0 1.0 0.01 100° C. × 86.2 2 2
    ple 13 less cone- 1 hr
    steel based
    sheet com-
    Compar- Stain- PET Al — — pound 60 100 160 8 29 3.4 6.8 1.0 0.01 100° C. × 85.9 3 2
    ative less Sili- 1 hr
    Exam- steel cone-
    ple 7 sheet based
    com-
    pound
    Compar- Stain- PET Al — — Sili- 120 100 220 11 29 3.6 11 1.0 0.01 100° C. × 85.4 4 3
    ative less cone- 1 hr
    Exam- steel based
    ple 8 sheet com-
    pound
    Compar- Stain- PET Al — — Sili- 300 100 390 19.5 29 3.8 15 1.0 0.01 100° C. × 85.6 4 4
    ative less cone- 1 hr
    Exam- steel based
    ple 9 sheet com-
    pound
    Exam- Cold- PET Al Silane ≦0.1 Sili- 100 130 30 2.0 0.01 1.0 0.01 100° C. × 86.7 2 2
    ple 14 rolled cou- cone- 1 hr
    steel pling based
    sheet agent com-
    pound
    Exam- Cold- PET Al Silane ≦0.1 Sili- 100 130 0.013 30 2.0 0.05 1.0 0.01 100° C. × 86.9 2 2
    ple 15 rolled cou- cone- 1 hr
    steel pling based
    sheet agent com-
    pound
    Exam- Cold- PET Al Silane ≦0.1 Sili- 100 130 0.13 30 2.0 0.1 1.0 0.01 100° C. × 88.5 1 2
    ple 16 rolled cou- cone- 1 hr
    steel pling based
    sheet agent com-
    pound
    Exam- Cold- PET Al Silane ≦0.1 Sili- 100 130 1.3 30 2.0 0.5 1.0 0.01 100° C. × 89.4 1 1
    ple 17 rolled cou- cone- 1 hr
    steel lingp based
    sheet agent com-
    pound
    Exam- Cold- PET Al Silane ≦0.1 Sili- 100 130 7.8 29 2.0 7.0 1.0 0.01 100° C. × 89.4 1 1
    ple 18 rolled cou- cone- 1 hr
    steel pling based
    sheet agent com-
    pound
    Exam- Cold- PET Al Silane ≦0.1 Sili- 100 130 9.1 28 2.0 10 1.0 0.01 100° C. × 89.4 1 1
    ple 19 rolled cou- cone- 1 hr
    steel pling based
    sheet agent com-
    pound
    Exam- Cold- PET Al Silane ≦0.1 Sili- 100 130 10.4 28 2.0 15 1.0 0.01 100° C. × 88.4 1 2
    ple 20 rolled cou- cone- 1 hr
    steel pling based
    sheet agent com-
    pound
    Exam- Cold- PET Al Silane ≦0.1 Sili- 100 130 13 28 2.0 20 1.0 0.01 100° C. × 85.1 2 2
    ple 21 rolled cou- cone- 1 hr
    steel pling based
    sheet agent com-
    pound
    Exam- Stain- PET Al — — Sili- 100 130 39 24 2.0 0.4 1.0 0.01 120° C. × 88.6 1 2
    ple 22 less cone- 24 hr
    steel based
    sheet com-
    pound
    Exam- Stain- PET Al — — Sili- 100 130 176 15 2.0 2.9 1.0 0.01 120 C. × 87.9 1 2
    ple 23 less cone- 24 hr
    steel based
    sheet com-
    pound
    Compar- Stain- PET Al — — Sili- 75 2.0 0.1 1.0 0.01 — 75.4 4 4
    ative less cone
    Exam- steel rubber
    ple 10 sheet
    Compar- Stain- PET Al — — Sili- 78 3.0 2.0 1.0 0.01 — 81.1 4 4
    ative less cone
    Exam- steel resin
    ple 11 sheet
    Compar- Stain- PET Al — — SiO2 100 4.0 90 0.1 0.01 — 89.9 3 4
    ative less Depo-
    Exam- steel sition
    ple 12 sheet film
    Compar- Stain- PET Al — — Boro- 60 4.0 70 10.0 0.01 — 86.6 3 4
    ative less silicate
    Exam- steel glass
    ple 13 sheet
    Compar- Stain- PET Al — — Metal 70 4.0 70 1.0 0.01 — 87.6 3 4
    ative less silicate
    Exam- steel
    ple 14 sheet
  • TABLE 2
    Protective layer Characteristics
    Interlayer SiO2 SiOn Elastic Re-
    Reflec- Thick- Con- Num- mod- Thick- Curing flec- Sand Weather
    Sub- Base tive ness A B C D E F G V W Other verted ber ulus ness Ra condi- tance resis- resis-
    strate layer layer Type μm Parts by mass % of n GPa μm μm tions (%) tance tance
    Exam- Stain- PET Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.7 1.0 0.01 100° C. × 88.7 1 1
    ple 24 less cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Stain- PET Al Tita- ≦0.1 Silicone- 100 130 6.5 29 2.0 3.1 1.0 0.01 100° C. × 87.6 1 1
    ple 25 less nium based 1 hr
    steel cou- compound
    sheet pling
    agent
    Exam- Stain- PET Al Zr ≦0.1 Silicone- 100 130 6.5 29 2.0 3.0 1.0 0.01 100° C. × 88.5 1 1
    ple 26 less cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Stain- PET Al Viny 0.5 Silicone- 100 130 6.5 29 2.0 2.6 1.0 0.01 100° C. × 86.2 1 1
    ple 27 less chloride based 1 hr
    steel acetate compound
    sheet resin
    Exam- Stain- PET Al Vinyl 1 Silicone- 100 130 6.5 29 2.0 2.6 1.0 0.01 100° C. × 85.8 1 1
    ple 28 less chloride based 1 hr
    steel acetate compound
    sheet resin
    Exam- Stain- PET Al Vinyl 2 Silicone- 100 130 6.5 29 2.0 2.6 1.0 0.01 100° C. × 83.4 1 1
    ple 29 less chloride based 1 hr
    steel acetate compound
    sheet resin
    Exam- Stain- PET Al Vinyl 5 Silicone- 100 130 6.5 29 2.0 2.6 1.0 0.01 100° C. × 81.1 1 1
    ple 30 less chloride based 1 hr
    steel acetate compound
    sheet resin
    Exam- Stain- PET Al Acrylic 0.5 Silicone- 100 130 6.5 29 2.0 3.3 1.0 0.01 100° C. × 86.1 1 1
    ple 31 less resin based 1 hr
    steel compound
    sheet
    Exam- Cold- PET Al — — Silicone- 100 130 6.5 29 2.0 2.6 1.0 0.01 100° C. × 89.7 1 2
    ple 32 rolled based 1 hr
    steel compound
    sheet
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.6 0.01 0.01 100° C. × 90.0 2 2
    ple 33 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.6 0.1 0.01 100° C. × 89.9 1 2
    ple 34 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.6 1.0 0.01 100° C. × 88.7 1 2
    ple 35 Rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.6 10.0 0.01 100° C. × 87.8 1 2
    ple 36 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.6 20.0 0.01 100° C. × 82.3 1 2
    ple 37 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 50 100 130 6.5 30 2.5 2.2 1.0 0.01 100° C. × 88.5 1 2
    ple 38 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 100 130 6.5 31 2.7 4.8 1.0 0.01 100° C. × 89.0 1 2
    ple 39 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 6.5 12 3.0 5.1 1.0 0.01 100° C. × 88.8 1 2
    ple 40 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 50 100 120 6 31 2.0 2.1 1.0 0.01 100° C. × 89.1 1 2
    ple 41 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 15 0.75 29 2.0 2.3 1.0 0.01 100° C. × 89.7 1 2
    ple 42 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.5 0.1 0.01 100° C. × 88.7 1 2
    ple 43 rolled (10 μm cou-\ based 1 hr
    steel thick- pling compound
    sheet ness) agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.4 0.1 0.01 100° C. × 90.2 1 2
    ple 44 rolled (100 μm cou- based 1 hr
    steel thick- pling compound
    sheet ness) agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.6 0.1 0.01 100° C. × 78.6 1 2
    ple 45 rolled (0.01 cou- based 1 hr
    steel μm pling compound
    sheet Thick- agent
    ness)
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.6 0.1 0.01 100° C. × 85.3 1 2
    ple 46 rolled (0.05 cou- based 1 hr
    steel μm pling compound
    sheet thick- agent
    ness)
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.6 0.1 0.01 100° C. × 88.4 1 2
    ple 47 rolled (0.2 cou- based 1 hr
    steel μm pling compound
    sheet thick- agent
    ness)
    Exam- Cold- PET Ag — — Silicone- 100 130 6.5 29 2.0 3.1 1.0 0.01 100° C. × 95.3 1 2
    ple 48 rolled based 1 hr
    steel compound
    sheet
    Exam- Cold- PET Ag Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.5 0.1 0.01 100° C. × 94.8 1 2
    ple 49 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- Glass Al Silane ≦0.1 Silicone- 100 130 6.5 29 2.0 2.6 10.0 0.01 100° C. × 90.1 1 2
    ple 50 rolled sheet cou- based 1 hr
    steel pling compound
    sheet agent
  • TABLE 3
    Protective layer Characteristics
    Interlayer SiO2 SiOn Elastic Re-
    Reflec- Thick- Con- Num- mod- Thick- Curing flec- Sand Weather
    Sub- Base tive ness A B C D E F G V W Other verted ber ulus ness Ra condi- tance resis- resis-
    strate layer layer Type μm Parts by mass % of n GPa μm μm tions (%) tance tance
    Exam- Plastic PET Al — — Silicone- 100 130 6.5 29 2.0 3.0 1.0 0.01 100° C. × 89.7 1 2
    ple 51 sub- based 1 hr
    strate compound
    Exam- Ceramic PET Al — — Silicone- 100 130 6.5 29 2.0 3.1 1.0 0.01 100° C. × 89.4 1 2
    ple 52 sub- based 1 hr
    strate compound
    Exam- Glass PET Al — — Silicone- 100 130 6.5 29 2.0 3.1 1.0 0.01 100° C. × 88.6 1 2
    ple 53 sub- based 1 hr
    strate compound
    Exam- Stain- Glass Al — — Silicone- 100 130 6.5 29 2.0 2.9 1.0 0.01 100° C. × 87.9 1 2
    ple 54 less coat based 1 hr
    steel compound
    sheet
    Exam- Stain- — Al — — Silicone- 100 130 6.5 29 2.0 2.9 1.0 0.02 100° C. × 75.4 1 2
    ple 55 less based 1 hr
    steel compound
    sheet
    Exam- Stain- PET Al — — Silicone- 100 130 6.5 29 2.0 3.1 1.0 0.05 100° C. × 85.1 1 2
    ple 56 less based 1 hr
    steel compound
    sheet
    Exam- Stain- PET Al — — Silicone- 100 130 6.5 29 2.0 3.0 1.0 0.10 100° C. × 81.2 1 2
    ple 57 less based 1 hr
    steel compound
    sheet
    Exam- Stain- PET Al — — Silicone- 100 130 6.5 29 2.0 3.1 1.0 0.30 100° C. × 75.4 1 2
    ple 58 less based 1 hr
    steel compound
    sheet
    Exam- Stain- PET Al — — Silicone- 100 130 6.5 29 2.0 2.9 1.0 0.50 100° C. × 71.0 1 2
    ple 59 less based 1 hr
    steel compound
    sheet
    Exam- Cold- — Melted Al — — Silicone- 100 130 6.5 29 2.0 2.6 1.0 0.01 100° C. × 84.7 1 2
    ple 60 rolled (having a based 1 hr
    steel thickness compound
    sheet of 80 μm
    by being
    subjected
    to mirror
    polishing)
    Compar- Stain- — — — — — — — 50.7 4 4
    ative less
    Exam- steel
    ple 15 sheet
    Compar- Cold- — — — — — — — 34.3 4 4
    ative rolled
    Exam- steel
    ple 16 sheet
    Exam- Hot-dip PET Al Silane ≦0.1 Silicone- 100 130 6.5 30 2.0 2.8 1.0 0.02 100° C. × 88.6 1 1
    ple 61 galva- cou- based 1 hr
    nized pling compound
    Exam- Hot-dip PET Al Silane ≦0.1 Silicone- 100 130 6.5 30 2.0 2.7 5.0 0.01 100° C. × 88.5 1 1
    ple 62 galva- cou- based 1 hr
    nized pling compound
    steel agent
    sheet
    Exam- Hot-dip PET Al #Silane ≦0.1 Silicone- 100 130 6.5 30 2.0 2.8 1.0 0.01 100° C. × 88.7 1 1
    ple 63 galva- cou- based 1 hr
    nized pling compound
    steel agent
    sheet
    Exam- electro- PET Al Silane ≦0.1 Silicone- 100 130 6.5 30 2.0 2.9 1.0 0.01 100° C. × 88.9 1 1
    ple 64 galva- cou- based 1 hr
    nized pling compound
    steel agent
    sheet
    Exam- electro- PET Al Silane ≦0.1 Silicone- 100 130 6.5 30 2.0 2.7 5.0 0.01 100° C. × 88.4 1 1
    ple 65 galva- cou- based 1 hr
    nized pling compound
    steel agent
    sheet
    Exam- electro- PET Al #Silane ≦0.1 Silicone- 100 130 6.5 30 2.0 2.7 1.0 0.01 100° C. × 88.7 1 1
    ple 66 galva- cou- based 1 hr
    nized pling compound
    steel agent
    sheet
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 0 30 2.0 0.01 1.0 0.01 100° C. × 86.7 2 2
    ple 67 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 0.013 30 2.0 0.05 1.0 0.01 100° C. × 86.9 2 2
    ple 68 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 7.8 X30 24 2.0 8.3 3.0 0.02 100° C. × 85.3 1 1
    ple 69 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 7.8 Y30 24 2.0 4.6 4.0 0.03 100° C. × 80.1 2 1
    ple 70 rolled cou- based 1 hr
    steel pling compound
    sheet agent
    Exam- Cold- PET Al Silane ≦0.1 Silicone- 100 130 7.8 Z30 24 2.0 7.9 5.0 0.10 100° C. × 72.1 2 1
    ple 71 rolled cou- based 1 hr
    steel pling compound
    sheet agent
  • TABLE 4
    Compounding agent
    A Tetramethoxysilane
    B 3-Glycidoxypropyltrimethoxysilane
    C Methyltrimethoxysilane
    D 3-Glycidoxypropylmethyldimethoxysilane
    E Dimethyldimethoxysilane
    F Trimethylsilyl chloride
    G
    1,4-Butanediol diglycidyl ether
    X Titanium oxide (rutile type, particle size 10 nm)
    Y Calcium carbonate (particle size 0.2 μm)
    Z Zirconium oxide (particle size 0.6 μm)
  • TABLE 5
    Curing agent
    V Diethylenetriamine
    W A mixture of methyl hexahydrophthalic
    anhydride:tris(dimethylaminomethyl)phenol = 99:1
  • As the results described in Tables 1 to 3 clearly show, we found that if a protective layer in which either or both of the Si content (expressed in terms of SiO2) and the Si-bound oxygen atom number are outside of a predetermined range is used, the reflectance can be maintained at a high value, but the sand resistance and weather resistance deteriorate (Comparative Examples 1 to 14).
  • On the other hand, we found that if a protective layer in which both the Si content (expressed in terms of SiO2) and the Si-bound oxygen atom number are within a predetermined range is used, the excellent reflectance of the reflective layer is maintained, and the sand resistance and weather resistance also become excellent (Examples 1 to 71).
  • Particularly, we found that in the solar reflector plates prepared in Examples 14 to 21, 24 to 31, 33 to 47, 49 to 50, and 61 to 71 in which a stainless steel sheet, a cold-rolled steel sheet, a hot-dip galvanized steel sheet, or an electrogalvanized steel sheet is used as a substrate, and the interlayer is provided between the reflective layer and protective layer, the sand resistance and weather resistance (particularly, weather resistance) tend to further improve.

Claims (17)

1-5. (canceled)
6. A solar reflector plate comprising:
a substrate;
a reflective layer provided onto the substrate; and
a protective layer provided onto the reflective layer,
wherein the protective layer contains silicon in an amount of 10% by mass to 60% by mass in terms of SiO2 and an organic substance, and has 1.5 to 3.2 oxygen atoms on average that form a chemical bond with silicon.
7. The solar reflector plate according to claim 6, wherein an elastic modulus of the protective layer is 0.1 GPa to 15 GPa.
8. The solar reflector plate according to claim 6, wherein the reflective layer contains aluminum and/or silver.
9. The solar reflector plate according to claim 6, further comprising an interlayer containing at least one selected from the group consisting of a silane coupling agent, a titanium coupling agent, a zirconium coupling agent, and an organic resin, between the reflective layer and the protective layer.
10. The solar reflector plate according to claim 6, further comprising at least one base layer constituted of an organic material and/or an inorganic material, between the substrate and the reflective layer.
11. The solar reflector plate according to claim 7, wherein the reflective layer contains aluminum and/or silver.
12. The solar reflector plate according to claim 7, further comprising an interlayer containing at least one selected from the group consisting of a silane coupling agent, a titanium coupling agent, a zirconium coupling agent, and an organic resin, between the reflective layer and the protective layer.
13. The solar reflector plate according to claim 8, further comprising an interlayer containing at least one selected from the group consisting of a silane coupling agent, a titanium coupling agent, a zirconium coupling agent, and an organic resin, between the reflective layer and the protective layer.
14. The solar reflector plate according to claim 11, further comprising an interlayer containing at least one selected from the group consisting of a silane coupling agent, a titanium coupling agent, a zirconium coupling agent, and an organic resin, between the reflective layer and the protective layer.
15. The solar reflector plate according to claim 7, further comprising at least one base layer constituted of an organic material and/or an inorganic material, between the substrate and the reflective layer.
16. The solar reflector plate according to claim 8, further comprising at least one base layer constituted of an organic material and/or an inorganic material, between the substrate and the reflective layer.
17. The solar reflector plate according to claim 9, further comprising at least one base layer constituted of an organic material and/or an inorganic material, between the substrate and the reflective layer.
18. The solar reflector plate according to claim 11, further comprising at least one base layer constituted of an organic material and/or an inorganic material, between the substrate and the reflective layer.
19. The solar reflector plate according to claim 12, further comprising at least one base layer constituted of an organic material and/or an inorganic material, between the substrate and the reflective layer.
20. The solar reflector plate according to claim 13, further comprising at least one base layer constituted of an organic material and/or an inorganic material, between the substrate and the reflective layer.
21. The solar reflector plate according to claim 14, further comprising at least one base layer constituted of an organic material and/or an inorganic material, between the substrate and the reflective layer.
US14/391,420 2012-04-12 2013-03-19 Solar reflector plate Active US9594191B2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2012-091286 2012-04-12
JP2012091286 2012-04-12
PCT/JP2013/057878 WO2013153923A1 (en) 2012-04-12 2013-03-19 Solar reflector

Publications (2)

Publication Number Publication Date
US20150109696A1 true US20150109696A1 (en) 2015-04-23
US9594191B2 US9594191B2 (en) 2017-03-14

Family

ID=49327496

Family Applications (1)

Application Number Title Priority Date Filing Date
US14/391,420 Active US9594191B2 (en) 2012-04-12 2013-03-19 Solar reflector plate

Country Status (8)

Country Link
US (1) US9594191B2 (en)
EP (1) EP2837958B1 (en)
JP (1) JP5994845B2 (en)
KR (1) KR20140125448A (en)
CN (1) CN104220905B (en)
ES (1) ES2778865T3 (en)
TW (1) TWI504503B (en)
WO (1) WO2013153923A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10054818B2 (en) 2014-07-08 2018-08-21 Sharp Kabushiki Kaisha Mirror plate and mirror display
US10879439B2 (en) * 2015-06-29 2020-12-29 Kuraray Co., Ltd. Polyamide composition for LED reflection plate, LED reflection plate, and light-emitting device including reflection plate

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015161826A (en) * 2014-02-27 2015-09-07 コニカミノルタ株式会社 Film mirror and reflection device for solar thermal power generation
US9728440B2 (en) 2014-10-28 2017-08-08 Globalfoundries Inc. Non-transparent microelectronic grade glass as a substrate, temporary carrier or wafer
WO2022019659A1 (en) * 2020-07-24 2022-01-27 주식회사 나노밸리 Solar cell reflective structure
KR102232231B1 (en) 2020-12-04 2021-03-24 이창무 Reflector plate solar panel

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5661536A (en) 1979-10-22 1981-05-27 Agency Of Ind Science & Technol Reflection type heat collecting plate and method of manufacturing and using the same
JPS574003A (en) 1980-06-11 1982-01-09 Toshiba Electric Equip Corp Solar energy absorber
US4343533A (en) * 1980-12-31 1982-08-10 Dow Corning Corporation Solar radiation reflector with a cellulosic substrate and method of making
JPS57125901A (en) 1981-01-29 1982-08-05 Sharp Corp Reflector and its production
GB9500330D0 (en) 1995-01-09 1995-03-01 Pilkington Plc Coatings on glass
US5677050A (en) 1995-05-19 1997-10-14 Minnesota Mining And Manufacturing Company Retroreflective sheeting having an abrasion resistant ceramer coating
EP1154289A1 (en) * 2000-05-09 2001-11-14 Alcan Technology & Management AG Reflector
JP2002348674A (en) * 2001-05-24 2002-12-04 Nisshin Steel Co Ltd Aluminum plated steel sheet superior in solar radiation reflectivity
WO2005081021A1 (en) 2004-02-24 2005-09-01 Matsushita Electric Works, Ltd. Light reflector and lighting fixture including the same
US20080302418A1 (en) * 2006-03-18 2008-12-11 Benyamin Buller Elongated Photovoltaic Devices in Casings
JP2007296691A (en) * 2006-04-28 2007-11-15 Konica Minolta Holdings Inc Gas barrier material, manufacturing method for gas barrier material, gas barrier material having transparent conductive film, and organic electroluminescent element
JP2010041040A (en) 2008-07-10 2010-02-18 Semiconductor Energy Lab Co Ltd Photoelectric conversion device and method of manufacturing the same
JP5471293B2 (en) 2008-10-23 2014-04-16 三菱化学株式会社 Heat ray reflective film, laminate thereof and coating solution for forming heat ray reflective layer
JP2011102348A (en) * 2009-11-10 2011-05-26 Kaneka Corp Curable composition and cured material thereof
JP5630497B2 (en) 2010-02-26 2014-11-26 旭硝子株式会社 Coating composition for solar heat collecting reflector, solar heat collecting reflector and method for producing the same
WO2011129411A1 (en) 2010-04-16 2011-10-20 旭硝子株式会社 Coating composition for coating surface of reflective plate for solar heat collection purposes, reflective plate for solar heat collection purposes, and processes for production of the coating composition and the reflective plate
JP5545006B2 (en) * 2010-04-20 2014-07-09 三菱化学株式会社 Heat ray reflective laminate and heat ray reflective layer protective layer forming composition
JP5471825B2 (en) * 2010-05-21 2014-04-16 三菱化学株式会社 Heat ray reflective laminate and heat ray reflective layer forming coating solution
JP2013199507A (en) 2010-07-14 2013-10-03 Asahi Glass Co Ltd Coating composition for coating surface of solar energy collecting reflector and method for producing solar energy collecting reflector
US20130206214A1 (en) * 2010-08-31 2013-08-15 Mitsubishi Plastics, Inc. Solar battery cover film for and solar battery module manufactured using same
WO2012057005A1 (en) 2010-10-27 2012-05-03 コニカミノルタオプト株式会社 Film mirror for solar power generation purposes, process for manufacturing film mirror for solar power generation purposes, and reflection device for solar power generation purposes
US20130293951A1 (en) 2011-01-19 2013-11-07 Konica Minolta , Inc. Film mirror and reflecting apparatus for solar power generation

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10054818B2 (en) 2014-07-08 2018-08-21 Sharp Kabushiki Kaisha Mirror plate and mirror display
US10879439B2 (en) * 2015-06-29 2020-12-29 Kuraray Co., Ltd. Polyamide composition for LED reflection plate, LED reflection plate, and light-emitting device including reflection plate

Also Published As

Publication number Publication date
TW201343382A (en) 2013-11-01
CN104220905A (en) 2014-12-17
EP2837958B1 (en) 2020-01-08
WO2013153923A1 (en) 2013-10-17
TWI504503B (en) 2015-10-21
JP5994845B2 (en) 2016-09-21
WO2013153923A8 (en) 2014-08-21
US9594191B2 (en) 2017-03-14
EP2837958A4 (en) 2015-07-08
KR20140125448A (en) 2014-10-28
CN104220905B (en) 2017-10-24
JPWO2013153923A1 (en) 2015-12-17
ES2778865T3 (en) 2020-08-12
EP2837958A1 (en) 2015-02-18

Similar Documents

Publication Publication Date Title
US9594191B2 (en) Solar reflector plate
US10209414B2 (en) Infrared-reflecting film
JP5480373B2 (en) Aircraft transparent material with solar control characteristics
US8586181B2 (en) Protective sheet for solar cell module
WO2013015112A1 (en) Mirror for solar light reflection, reflection device for solar-heat power generation, functional film, and electrostatic charge preventing composition for outdoor use
CN108152871B (en) Silver-plated reflecting film
JP7013736B2 (en) A composition for forming a primer layer, a barrier film, a wavelength conversion sheet, and a method for producing a wavelength conversion sheet.
KR20120121363A (en) Back sheet for solar cell module and solar cell module comprising the same
KR20230152165A (en) Optical laminate and wavelength conversion sheet
KR20120059277A (en) Glass for vehicle
JP2000141531A (en) Solar battery cover film and its manufacture, and solar battery module using the cover film
JP2005144719A (en) Gas barrier composite film excellent in weatherability
JP2006095783A (en) Transparent gas barrier film and substrate for display using it
TWI513591B (en) Protective film
WO2017033872A1 (en) Heat ray-reflecting material, window, and method for thermally insulating window
JP7238767B2 (en) Transparent conductive gas barrier laminate and device comprising the same
US20180275327A1 (en) Light-transmitting laminate and method for producing light-transmitting laminate
JP2014214986A (en) Mirror for solar thermal power generation and reflection device for solar thermal power generation equipped with the same
JP2012158821A (en) Method for producing thin film and vapor deposition material for co-vapor deposition for forming thin film, thin film obtained by the method, thin film sheet having the thin film, and laminated sheet
US10076891B2 (en) Barrier film and method for manufacturing same
KR20170017125A (en) Gas and moisture barrier coating composition for forming a barrier film coating layer and gas and moisture barrier film using the same
WO2013180202A1 (en) Functional film and method for producing functional film
JP2016224076A (en) Film mirror and solar heat reflecting light reflection device using the film mirror
JP2010212341A (en) Solar cell back sheet
EP3360680A2 (en) Laminated material for vacuum insulation panel cover material, and vacuum insulation panel cover material comprising same

Legal Events

Date Code Title Description
AS Assignment

Owner name: JFE STEEL CORPORATION, JAPAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SASHI, KAZUMICHI;OSHIGE, TAKAHIKO;ISHIKAWA, SHIN;AND OTHERS;REEL/FRAME:033919/0651

Effective date: 20140910

STCF Information on status: patent grant

Free format text: PATENTED CASE

MAFP Maintenance fee payment

Free format text: PAYMENT OF MAINTENANCE FEE, 4TH YEAR, LARGE ENTITY (ORIGINAL EVENT CODE: M1551); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

Year of fee payment: 4

MAFP Maintenance fee payment

Free format text: PAYMENT OF MAINTENANCE FEE, 8TH YEAR, LARGE ENTITY (ORIGINAL EVENT CODE: M1552); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

Year of fee payment: 8